# N844QS: 2023 Textron 700 - Status: Valid registration - Airframe: [Textron 700](https://openairdocs.org/model/textron-700) (registry code 2076819, 14 seats) - Engine: [Honeywell AS907-2-1S](https://openairdocs.org/engine/honeywell-as907-2-1s) (registry code 33403) - Data sheets: [TCDS T00015WI](https://openairdocs.org/tcds/T00015WI) (Textron Aviation Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 700-0093 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 19, 2023 - Certificate issued: August 22, 2024 - Expires: August 31, 2031 - Mode S code: AB9024 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=844QS - Page: https://openairdocs.org/aircraft/N844QS From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 2 in force ### Matched by airframe (Textron 700) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 ### Matched by engine (Honeywell AS907-2-1S) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N844QS. ## FAA accident and incident reports None matched to N844QS. ## Service difficulty reports (3) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2024120401383](https://openairdocs.org/sdr/DXTA2024120401383), Dec 2, 2024: WIRE HARNESS. DEFECTIVE. MAIN ENTRY DOOR HANDLE, UNABLE TO OPEN IT IS BINDING REMOVED AND REPLACED MCD THRESHOLD WIRE HARNESS ASSEMBLY. DOOR OPS CHECKS GOOD. REF. CESSNA CE-700 LONGITUD - [SDR DXTA2024092000595](https://openairdocs.org/sdr/DXTA2024092000595), Sep 18, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTING: EMER LIGHTS DO NOT ILLUMINATE IN THE ON POSITION WHEN NO DC POWER IS AVAILABLE. LIGHTS WORK NORMALLY IN THE ARMED POSITION REGARDLESS OF DC - [SDR DXTA2024090520419](https://openairdocs.org/sdr/DXTA2024090520419), Sep 2, 2024: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHT BATTERY NOT HOLDING A CHARGE. ANYTIME AIRCRAFT IS SHUT DOWN MORE THAN 90 MINUTES ALL EMERG LIGHTS WILL NOT ILLUMINATE UNTIL CHARGING BATTERIES F ## Service difficulty reports on N844QS not matched to an aircraft (18) They name N844QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2016032506218](https://openairdocs.org/sdr/DXTA2016032506218), Mar 24, 2016: UNKNOWN. ODOR. AT FL400 WE TURNED THE DEFOG FAN ON & SMELLED AN ELEC OR PLASTIC BURNING SMELL. TURNED THE DEFOG FAN OFF IMMEDIATELY & THE SMELL DISSIPATED. REMOVED FLOOR PANEL - [SDR DXTA2016032506217](https://openairdocs.org/sdr/DXTA2016032506217), Mar 24, 2016: UNKNOWN. ODOR. AT FL400 WE TURNED THE DEFOG FAN ON & SMELLED AN ELEC OR PLASTIC BURNING SMELL. WE TURNED THE DEFOG FAN OFF IMMEDIATELY & THE SMELL DISSIPATED. REMOVED FLOOR PA - [SDR DXTA2015110506116](https://openairdocs.org/sdr/DXTA2015110506116), Nov 5, 2015: SWITCH. UNSERVICEABLE. AT FL 380 IN THE CLIMB, TWO LOUD BANGS, EMER PRESS & ACM OVHT LIGHT CAME ON. CABIN WAS -3700 FPM. STARTED EMER DECENT, AFTER 1 MIN CABIN STARTED PRESSURIZING. T - [SDR DXTA2014042105738](https://openairdocs.org/sdr/DXTA2014042105738), Apr 19, 2014: SWITCH. FAULTED. AFTER TAKEOFF & CLIMBING THROUGH 400 FT, LEFT THRUST REVERSER ARM LIGHT & HYD PRESSURE ANNUNCIATOR ILLUMINATED. IAW THE CHECKLIST, THE LT EMERGENCY STOW SWITCH - [SDR DXTA2012100805137](https://openairdocs.org/sdr/DXTA2012100805137), Oct 5, 2012: WHEEL. UNSERVICEABLE. DURING TAXI, A SHIMMY/VIBRATION IS FELT BETWEEN 15-20KTS. IT FEELS LIKE A "POOR CONDITION" TAXIWAY SURFACE. THERE IS NO NOTICABLE DIRECTIONAL BIAS AND ALL HANDL - [SDR DXTR20120124008](https://openairdocs.org/sdr/DXTR20120124008), Jan 24, 2012: LINE. CHAFED. FUEL TRANSFER LINE, PN 6526400-61, IS CHAFING THE FUSELAGE UNDER PANEL 161AB. - [SDR DXTA2011092604735](https://openairdocs.org/sdr/DXTA2011092604735), Sep 25, 2011: AILERON SYS. RATCHETING. AILERON JERKY IN FLIGHT WITH AUTOPILOT OFF. SMOOTH ON GROUND WITH POWER OFF. RESHIMMED PILOTS CONTROL YOKE DRUM ASSY. ADJUSTED RT AILERON QUADRANT GAP TO ACCEPT - [SDR CWQR201006](https://openairdocs.org/sdr/CWQR201006), Dec 14, 2010: DOOR. STUCK. (CWQR) DURING A SCHEDULED MX EVENT, THE EMERGENCY EXIT DOOR WAS REMOVED. REMOVAL OF THE EMERGENCY EXIT DOOR WAS FOUND TO BE VERY DIFFICULT. REQUIRED 2 TECHS AND - [SDR 2010F00036](https://openairdocs.org/sdr/2010F00036), Feb 11, 2010: WARNING LIGHT. ILLUMINATED. ON APPROACH, EXT FLAPS TO 15, HYD PUMP REMAINED ILLUMINATED. REPOSITIONED FLAPS AND THE LIGHT REMAINED ON. IMMEDIATELY EXT GEAR AND FULL FLAPS. THE HYD LIGHT EX - [SDR DXTA2009063003710](https://openairdocs.org/sdr/DXTA2009063003710), Jun 28, 2009: THROTTLE CABLE. FRAYED. WHEN ATTEMPTING TO ADJUST POWER AFTER TURNING ANTI-ICE ON AT FL450, THE RT PWR LEVER WAS STUCK AND WOULD NOT MOVE FWD OR BACKWARD. ON DESCENT AND UPON REACHING - [SDR DXTA2009020403487](https://openairdocs.org/sdr/DXTA2009020403487), Feb 4, 2009: WIRE HARNESS. MALFUNCTIONED. ANTI SKID INOP LIGHT CAME ON DURING TAXI. WHILE TRYING TO STOP PLANE IT VEERED OFF TO THE LT LIKE 1 BRAKE WAS NOT WORKING. T/S ANTI-SKID SYS IAW AMM 32-42-00 AW - [SDR DXTA2009020303487](https://openairdocs.org/sdr/DXTA2009020303487), Feb 4, 2009: BRAKE ASSY. MALFUNCTIONED. ANTI SKID INOP LIGHT CAME ON DURING TAXI. WHILE TRYING TO STOP PLANE IT VEERED OFF TO THE LT LIKE 1 BRAKE WAS NOT WORKING. - [SDR DXTA200808183234](https://openairdocs.org/sdr/DXTA200808183234), Aug 18, 2008: O-RING. LEAKING. LOSS OF BRAKES ON TAXI INTO PARKING WITH LOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS. REQUIRED USE OF EMERGENCY BRAKES. UPON INSPECTION FLUID WAS LEAKING FROM - [SDR DXTA200803234](https://openairdocs.org/sdr/DXTA200803234), Aug 18, 2008: BRAKE. INOPERATIVE. LOSS OF BRAKES ON TAXI INTO PARKING. REQUIRED USE OF EMERGENCY BRAKES. (S) - [SDR DXTA200702495](https://openairdocs.org/sdr/DXTA200702495), Sep 23, 2007: WARNING LIGHT. ILLUMINATED. EMER PRESS CAME ON DURING TAKEOFF AND WAS WITHOUT AN ANNUNCIATOR. COULD HEAR THE "RUSHING AIR" SOUND WHEN THE THROTTLES WERE POWERED UP. RAN A/C FOR 30 MINUTES - [SDR DXTA200702332](https://openairdocs.org/sdr/DXTA200702332), Jul 12, 2007: INDICATOR. MALFUNCTIONED. LT MAIN LANDING GEAR INDICATOR WOULD NOT EXTINGUISH AFTER GEAR WAS BROUGHT UP. CYCLED GEAR 3 TIMES, INDICATOR STAYED ON EACH TIME. [07-23-07] JACKED A/C IAW CES - [SDR DXTA200702123](https://openairdocs.org/sdr/DXTA200702123), Apr 20, 2007: FCU. MALFUNCTIONED. LT ENGINE WOULD NOT DEVELOP FULL POWER FOR TAKEOFF. MAX POWER DEVELOPED WAS APPROXIMATELY 2 PERCENT N1 LOW, RIGHT ENGINE DEVELOPED FULL POWER. [SUP 05-02-07] VE - [SDR DXTA200501110](https://openairdocs.org/sdr/DXTA200501110), Nov 23, 2005: FUEL FILTER. BYPASSING. PRIOR TO 70 KTS DURING TAKEOFF ROLL THE LEFT FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED & THE TAKEOFF WAS ABORTED. INSPECTED BOTH LEFT AND RIGHT WING TANKS. REM ## STCs that may be installed (OpenAirDocs) (11) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Textron 700) - [STC ST12145SE](https://openairdocs.org/stc/ST12145SE): Installation of Starlink Aviation System. AeroMech Incorporated - [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC - [STC ST00415BO](https://openairdocs.org/stc/ST00415BO): Installation of an NVIS/NVG compatible lighting system and infrared capable exterior lighting. ATI Engineering Services LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST02812LA](https://openairdocs.org/stc/ST02812LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc - [STC ST04572CH](https://openairdocs.org/stc/ST04572CH): Installation of an Airborne Terminal System and a Ka Radome. StandardAero Business Aviation Services LLC - [STC ST02746SE](https://openairdocs.org/stc/ST02746SE): Installation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systems. Textron Aviation Inc - [STC ST02694SE](https://openairdocs.org/stc/ST02694SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval. AeroMech Incorporated - [STC ST04211NY](https://openairdocs.org/stc/ST04211NY): Installation of of NSM UNIFIS 3000 G2 Flight Inspection System. Aerospace Design & Compliance LLC - [STC ST01971WI](https://openairdocs.org/stc/ST01971WI): Installation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration Updates. Textron Aviation Inc - [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc ## Related - Other Textron 700 aircraft: https://openairdocs.org/model/textron-700/aircraft.md - The Honeywell AS907-2-1S engine: https://openairdocs.org/engine/honeywell-as907-2-1s.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.